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Effect of stress ratio on fatigue-crack growth in 7075-t6 aluminum-alloy sheet
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Stress ratio effect on axial load fatigue and crack propagation tests on aluminum alloy sheets |
| File Size | 1353055 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19680018001 |
| Archival Resource Key | ark:/13960/t89h0d48k |
| Language | English |
| Publisher Date | 1967-01-01 |
| Access Restriction | Open |
| Subject Keyword | Materials, Metallic Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |